1. J.J. Choury, Carbon-Carbon Materials for nozzles of solid propellant rocket motors AIAA paper 76-609. 12th Propulsion Conference - PALO ALTO, CA. July26-29,1976.
2. AIAA Technical Paper 92-3551. "Hot Gas Thrust Vector Control Motor." Michel Berdoyes, SEP, France and Russell A. Ellis, CSD, USA. Presented at28thAIAA/ASME/SAE/ASEE Joint Propulsion Conference, Nashville, TN, July6-8,1992.
3. AIAA Technical Paper 97-2672. "Development of a Carbon-Carbon Translating Nozzle Extension fortheRL10B-2 Liquid Rocket Engine." R. A. Ellis, J. C. Lee, and F. M. Payne, CSD, USA and M. Lacoste, A. Lacombe, and P. Joyez, SEP, France. Presented at33rdAIAA/ASME/SAE/ASEE Joint Propulsion Conference, Seattle, WA, July6-9,1997.
4. IAF TechnicalPaper IAF-97-S.2.04. "Carbon-Carbon Extendible Nozzles." M. Lacoste, A. Lacombe, and P. Joyez, SEP, France and R. A. Ellis, J. C. Lee, and F.M. Payne, CSD, USA. Presented at48thInternational Astronautical Congress, Turin, Italy, October6-10,1997.
5. AIAA Technical Paper 98-3363. "Testing of the RL10B-2 Carbon-Carbon Nozzle Extension." R. A. Ellis, J. C. Lee, and F. M. Payne, CSD, USA and M. Lacoste, A. Lacombe, and P. Joyez, SEP, France. Presented at34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Cleveland, OH, July13-15,1998.